A. Aghababaie and R. Theunissen, Modeling Free Shock Separation Induced Side Loads in Overexpanded Rocket Nozzles, AIAA Journal, vol.53, issue.1, pp.93-103, 2015.

M. B. Alkislar, A. Krothapalli, and L. M. Lourenco, Structure of a screeching rectangular jet : a stereoscopic particle image velocimetry study, Journal of Fluid Mechanics, vol.489, pp.121-154, 2003.

W. J. Baars and C. E. Tinney, Transient wall pressures in an overexpanded and large area ratio nozzle, Experiments in fluids, vol.54, issue.2, pp.1-17, 2013.

W. J. Baars, C. E. Tinney, J. H. Ruf, A. M. Brown, and D. M. Mcdaniels, Wall pressure unsteadiness and side loads in overexpanded rocket nozzles, AIAA Journal, vol.50, issue.1, pp.61-73, 2012.

W. J. Baars, J. H. Ruf, and C. E. Tinney, Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient, Experiments in Fluids, vol.56, issue.5, p.92, 2015.

P. Carriere, M. Sirieix, and J. Solignac, Similarity properties of the laminar or turbulent separation phenomena in a non-uniform supersonic flow, Proceedings of the 12th International Congress of Applied Mechanics, p.145157, 1968.

D. R. Chapman, D. M. Kuehn, and H. K. Larson, Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, 1958.

N. T. Clemens and V. Narayanaswamy, Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions, Annu. Rev. Fluid Mech, vol.46, pp.469-492, 2014.

S. Deck and A. T. Nguyen, Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Regime, AIAA journal, vol.42, issue.9, pp.1878-1888, 2004.
URL : https://hal.archives-ouvertes.fr/hal-00146838

J. Délery, Ecole nationale supérieure de l'aéronautique et de l'espace, 1998.

G. Dumnov, Unsteady Side-Loads Acting on the Nozzle with Developed Separation Zone, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp.1-8, 1996.

P. Dupont, C. Haddad, and J. F. Debiève, Space and time organization in a shock-induced separated boundary layer, Journal of Fluid Mechanics, vol.559, issue.255, 1986.

J. H. Gao and X. D. Li, A multi-mode screech frequency prediction formula for circular supersonic jets, The Journal of the Acoustical Society of America, vol.127, issue.3, pp.1251-1257, 2010.

A. Georges-picot, A. Hadjadj, and J. Herpe, Influence of downstream unsteadiness on shock pattern in separated nozzle flows, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, p.4000, 2014.

G. Hagemann, M. Terhardt, M. Frey, P. Reijasse, M. Onofri et al., Flow separation and side-loads in rocket nozzles, 4th International Symposium on Liquid Space Propulsion, 2000.

F. Q. Hu, The acoustic and instability waves of jets confined inside an acoustically lined rectangular duct, 1993.

M. R. Lammari, Mesures par vélocimétrie laser doppler dans une couche de mlange turbulente supersonique : quelques aspects du processus de mesure, 1996.

C. Y. Loh and K. B. Zaman, Numerical investigation of transonic resonance with a convergentdivergent nozzle, AIAA journal, vol.40, issue.12, pp.2393-2401, 2002.

S. Marié, S. Deck, and P. E. Weiss, From pressure fluctuations to dynamic loads on axisymmetric step flows with minimal number of kulites, Computers & Fluids, vol.39, issue.5, pp.747-755, 2010.

L. H. Nave and G. A. Coffey, Sea level side loads in high-area-ratio rocket engines, AIAA Paper, pp.73-1284, 1973.

A. T. Nguyen, Décollement Instationnaire et Charges Latérales dans les Tuyères Propulsives, 2003.

T. D. Norum, Screech suppression in supersonic jets, AIAA Journal, vol.21, issue.2, pp.235-240, 1983.

H. Oertel, Mach wave radiation of hot supersonic jets, Mechanics of Sound Generation in Flows, vol.1, pp.275-281, 1979.

H. Oertel, Mach wave radiation of hot supersonic jets investigated by means of a shock tube and new optical techniques, Proceedings of the 12th International Symposium on Shock-Tubes and Waves, Jerusalem. DTIC Document, 1980.

H. Oertel, Coherent structures producing machwaves inside and outside of the supersonic jet, Structure of Complex Turbulent Shear Flow, pp.334-343, 1983.

J. Östlund, Flow processes in rocket engine nozzles with focus on flow separation and side-loads, KTH, 2002.

J. Östlund and B. Muhammad-klingmann, Supersonic flow separation with application to rocket engine nozzles, Applied Mechanics Reviews, vol.58, issue.3, pp.143-177, 2005.

J. Panda, An experimental investigation of screech noise generation, Journal of Fluid Mechanics, vol.378, pp.71-96, 1999.

S. Piponniau, J. P. Dussauge, J. Debiève, and P. Dupont, A simple model for low-frequency unsteadiness in shock-induced separation, Journal of Fluid Mechanics, vol.629, 2009.
URL : https://hal.archives-ouvertes.fr/hal-01454909

K. J. Plotkin, Shock wave oscillation driven by turbulent boundary-layer fluctuations, AIAA Journal, vol.13, issue.8, pp.1036-1040, 1975.

J. Poggie and A. J. Smits, Experimental evidence for Plotkin model of shock unsteadiness in separated flow, Physics of Fluids, vol.17, issue.1, 2005.

A. Powell, On the mechanism of choked jet noise, Proceedings of the Physical Society. Section B, vol.66, issue.12, p.1039, 1953.

G. Raman, Supersonic jet screech: half-century from powell to the present, Journal of Sound and Vibration, vol.225, issue.3, pp.543-571, 1999.

F. Sartor, C. Mettot, R. Bur, and D. Sipp, Unsteadiness in transonic shock-wave/boundary-layer interactions: experimental investigation and global stability analysis, Journal of Fluid Mechanics, vol.781, pp.550-577, 2015.
URL : https://hal.archives-ouvertes.fr/tel-01018720

F. Scarano, Iterative image deformation methods in piv, Meas. Sci. Tech, vol.13, pp.1-19, 2002.

R. H. Schmucker, Flow process in overexpanded chemical rocket nozzles part 1: Flow separation. Nasa Tech, 1973.

R. H. Schmucker, Flow process in overexpanded chemical rocket nozzles part 2: Side loads due to asymetric separation, Nasa Tech, 1973.

R. Stark, Flow separation in rocket nozzles -an overview, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013.

R. Stark and C. Génin, Flow separation in rocket nozzles under high altitude condition, Shock Waves, vol.27, issue.1, pp.63-68, 2017.

R. Stark and B. Wagner, Experimental study of boundary layer separation in truncated ideal contour nozzles, Shock Waves, vol.19, issue.3, pp.185-191, 2009.

R. H. Stark, Flow separation in rocket nozzles, a simple criteria, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005.

P. J. Strykowski, A. Krothapalli, and S. ,

. Jendoubi, The effect of counterflow on the development of compressible shear layers, J. of Fluid Mech, vol.63, pp.1096-1100, 1996.

C. K. Tam and F. Q. Hu, On the three families of instability waves of high-speed jets, Journal of Fluid Mechanics, vol.201, pp.447-483, 1989.

C. K. Tam, J. M. Seiner, and J. C. Yu, Proposed relationship between broadband shock associated noise and screech tones, Journal of Sound and Vibration, vol.110, issue.2, pp.309-321, 1986.

M. Terhardt, G. Hagemann, and M. Frey, Flow separation and side-load behavious of truncated ideal rocket nozzles, AIAA Journal, 2006.

E. Touber and N. D. Sandham, Low-order stochastic modelling of low-frequency motions in reflected shock-wave/boundary-layer interactions, vol.671, 2011.

S. Verma, R. Stark, and H. Oskar, Relation between shock unsteadiness and the origin of side-loads inside a thrust optimized parabolic rocket nozzle, Aerospace Science and Technology, pp.474-483, 2006.

S. H. Walker and F. O. Thomas, Experiments characterizing nonlinear shear layer dynamics in a supersonic rectangular jet undergoing screech, Physics of Fluids, vol.9, issue.9, pp.2562-2579, 1994.

J. Westerweel and F. Scarano, Universal outlier detection for piv data, Experiments in Fluids, vol.39, issue.6, pp.1096-1100, 2005.

K. B. Zaman, M. D. Dahl, T. J. Bencic, and C. Y. Loh, Investigation of a transonic resonancewith convergent-divergent nozzles, Journal of Fluid Mechanics, vol.463, pp.313-343, 2002.

E. Zukoski, Turbulent boundary-layer separation in front of a forward-facing step, AIAA journal, vol.5, pp.1746-1753, 1967.